Overview
The MAD FLUXER Matt Pro 21×6.3 is a carbon fiber propeller designed for 21-inch class propulsion setups, featuring a polished/matt surface treatment and supplied with mounting accessories for common hub interfaces.
Key Features
- High quality carbon fiber + resin construction
- Polished/matt surface treatment
- Marked FLUXER PRO 21 x 6.3 CCW on the blade
- Includes cover plates, adapter rings, and M3 mounting screws
Specifications
| Model | FLUXER Matt Pro 21×6.3 in PROP |
|---|---|
| Size | 533.4 x 160 mm |
| Material | High quality carbon fiber+Resin |
| Single Weight | 58 g |
| Surface Treatment | Polished/matt |
| Optimum RPM | 2900-5500RPM/min |
| Single Thrust Limitation | 11 kg |
| Working Temp | -40C~65C |
| Storage Temp | -10C~50C |
| Storage Humidity | <85% |
| Package | Color box |
Propeller Mounting Hole
| Center bore | 12 mm |
|---|---|
| Screw holes | M3 |
| Hole spacing | 16 mm |
Test Data
| RPM | Thrust (gf) | Torque (N*m) | Output Power (W) | Efficiency (gf/W) |
|---|---|---|---|---|
| 933 | 120 | 0.0 | 3.6 | 33.92 |
| 1854 | 500 | 0.1 | 26.9 | 18.75 |
| 2657 | 1150 | 0.3 | 77.7 | 14.84 |
| 3499 | 1920 | 0.5 | 181.6 | 10.58 |
| 4191 | 2830 | 0.7 | 305.7 | 9.26 |
| 4970 | 3890 | 1.0 | 514.4 | 7.56 |
| 5613 | 4920 | 1.3 | 732.0 | 6.72 |
| 6197 | 6000 | 1.5 | 995.5 | 6.03 |
| 6673 | 7000 | 1.8 | 1263.1 | 5.54 |
| 7087 | 7850 | 2.1 | 1521.5 | 5.16 |
Recommended Config
| Propeller | ESC | Motor | Throttle | Thrust (g) |
|---|---|---|---|---|
| FLUXER Matt Pro 21×6.3 IN PROP | AMPX 40A HV | MAD M6C06 EEE KV140 | 50-60% | 1300-1800g / Motor (12S) |
| FLUXER Matt Pro 21×6.3 IN PROP | AMPX 40A HV / 60A HV | MAD M6C12 IPE V3 KV170 | 50-60% | 2000-3000g / Motor (12S) |
Whats Included
- 21×6.3 propellers: 2 pcs
- Cover Plate: 2 pcs
- 6/4 adapter ring: 2 pcs
- Hex Socket Cap Head Screw M3*12: 4 pcs
For compatibility checks (ESC/motor matching, mounting fit, and spares), contact [email protected] or visit https://rcdrone.top/.
Details
The FLUXER Pro Matt 21×6.3in propeller spec sheet includes key dimensions, mounting-hole details, and thrust/test data for setup planning.





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